CN110239726A - A method of for internally burying the oiling of magazine Aircraft Air plus bullet - Google Patents
A method of for internally burying the oiling of magazine Aircraft Air plus bullet Download PDFInfo
- Publication number
- CN110239726A CN110239726A CN201910398380.1A CN201910398380A CN110239726A CN 110239726 A CN110239726 A CN 110239726A CN 201910398380 A CN201910398380 A CN 201910398380A CN 110239726 A CN110239726 A CN 110239726A
- Authority
- CN
- China
- Prior art keywords
- aircraft
- magazine
- transmission mechanism
- oiling
- fuel charger
- Prior art date
- Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
- Pending
Links
- 238000000034 method Methods 0.000 title claims abstract description 29
- 230000005540 biological transmission Effects 0.000 claims abstract description 62
- 239000000446 fuel Substances 0.000 claims abstract description 40
- 230000007246 mechanism Effects 0.000 claims description 58
- 239000003921 oil Substances 0.000 claims description 21
- 230000008569 process Effects 0.000 claims description 7
- 230000000694 effects Effects 0.000 claims description 3
- 230000009471 action Effects 0.000 claims description 2
- 239000000295 fuel oil Substances 0.000 claims description 2
- 239000013589 supplement Substances 0.000 abstract description 4
- 210000001015 abdomen Anatomy 0.000 description 3
- 238000003032 molecular docking Methods 0.000 description 3
- 238000010586 diagram Methods 0.000 description 2
- 238000005516 engineering process Methods 0.000 description 2
- 238000004064 recycling Methods 0.000 description 2
- RZVHIXYEVGDQDX-UHFFFAOYSA-N 9,10-anthraquinone Chemical compound C1=CC=C2C(=O)C3=CC=CC=C3C(=O)C2=C1 RZVHIXYEVGDQDX-UHFFFAOYSA-N 0.000 description 1
- 230000008485 antagonism Effects 0.000 description 1
- 230000003471 anti-radiation Effects 0.000 description 1
- 230000009286 beneficial effect Effects 0.000 description 1
- 230000008602 contraction Effects 0.000 description 1
- 230000008878 coupling Effects 0.000 description 1
- 238000010168 coupling process Methods 0.000 description 1
- 238000005859 coupling reaction Methods 0.000 description 1
- 230000007812 deficiency Effects 0.000 description 1
- 229940079593 drug Drugs 0.000 description 1
- 239000003814 drug Substances 0.000 description 1
- 239000002828 fuel tank Substances 0.000 description 1
- 230000006872 improvement Effects 0.000 description 1
Classifications
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENT OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
- B64D39/00—Refuelling during flight
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENT OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
- B64D7/00—Arrangements of military equipment, e.g. armaments, armament accessories, or military shielding, in aircraft; Adaptations of armament mountings for aircraft
Landscapes
- Engineering & Computer Science (AREA)
- Aviation & Aerospace Engineering (AREA)
- Aiming, Guidance, Guns With A Light Source, Armor, Camouflage, And Targets (AREA)
Abstract
The invention discloses a kind of methods for internally burying the oiling of magazine Aircraft Air plus bullet, the connection of oil circuit is carried out between fuel charger and target aircraft using the pipeline of rigidity, the transmission of guided missile is used for outside rigid conduit, rigid conduit is stretching structure, it is stretched out by fuel charger and is connected to target aircraft, the transmission of guided missile is completed while carrying out oil transportation；Purpose is to add missile-borne machine to be connected with operational aircraft magazine oiling by refueling plus playing bracket, it realizes air refuelling and adds bullet or change spring operation work, it improves operational aircraft attack scale and executes task type and quantity, it is different from conventional aerial oiling mode, the present invention has adds resilience energy power in the air, it can be to bury magazine ammunition specification and quantity etc. in operational aircraft supplement, can be to bury magazine ammunition specification and quantity etc. in operational aircraft is replaced, long distance can be provided for operational aircraft and fighted one battle after another ability.
Description
Technical field
The present invention relates to air refuelling fields, more particularly, to kind for internally burying the side of the oiling of magazine Aircraft Air plus bullet
Method.
Background technique
The fight capabilities such as voyage, the bullet-loading capacity of most aviation aircrafts are mainly limited by take-off weight, therefore mostly use sky
Middle fuel charger carries out air refuelling, the long-distance flight ability of Lai Tigao operational aircraft.Meanwhile the following advanced fighter or bombing
Machine, which is all made of in abdomen, buries magazine design, and the weapons such as guided missile, bomb are packed into abdomen and are buried in magazine, open magazine in attack
Hatch door carries out throwing dispensing or transmitting, to improve stealthy prominent anti-and antagonism.The deficiency of this weaponry and combat mode
Be in:
1) magazine is buried in and carries bullet limited amount, is difficult to fight one battle after another.Magazine design, bulk are buried in abdomen due to using
Magazine is buried in limited size, especially first chance fighter plane to be only capable of loading the weapons such as several pieces of guided missiles, to carry out more attack in force,
The landing filling ammunition that need to make a return voyage is attacked again；
2) magazine is buried in and carries bullet limited types, is difficult to adapt to combat duty variation.The weapons such as modern guided missile are many kinds of, as in away from
Air-to-air missile, long range air to air missile, Cruise Missile, gliding bullet, antiradiation bullet, precision-guided bomb etc., different combat duties need
Carry difference ammunition, categories of operations, which changes, need to make a return voyage landing and replace ammunition；
3) magazine is buried in and carries bullet limited types, is difficult to carry out a variety of combat duties.It, often can only be into since aircraft bullet-loading capacity is limited
The single combat duty of row, and the bullet-loading capacity that a variety of combat duties need is larger and also big to the requirement of magazine size；
Existing tanker aircraft is only capable of providing flight refueling capability, is only capable of improving the cruising ability and long-range operation energy of aircraft
Power, and the attack scale and execution task type and quantity that aircraft itself bullet-loading capacity directly determines.
Summary of the invention
The purpose of the present invention is proposing a kind of improvement on the basis of existing air refuelling technology, can refuel simultaneously
In the case where, it can internally bury the supply that magazine aircraft carries out ammunition.
In order to realize above scheme, the present invention adopts the following technical scheme:
A method of for internally burying the oiling of magazine Aircraft Air plus bullet, when being met in the sky with target aircraft by fuel charger,
The connection of oil circuit is carried out between fuel charger and target aircraft using the pipeline of rigidity, the transmission of guided missile is used for outside rigid conduit,
Rigid conduit is stretching structure, is stretched out by fuel charger and is connected to target aircraft, and the biography of guided missile is completed while carrying out oil transportation
It is defeated.
In the above-mentioned technical solutions, the rigid pipeline include one it is that pipeline external is set with pipeline it is equidirectional into
The flexible strut of row, strut and pipeline constitute the bracket for being used for transmission guided missile.
In the above-mentioned technical solutions, the rigid pipeline includes the flexible tubing being arranged in pipeline.
In the above-mentioned technical solutions, described rigid pipeline one end has for positioning fixation with target aircraft oil inlet
Port.
In the above-mentioned technical solutions, it is provided with transmission mechanism on the bracket, retaining mechanism use is provided on transmission mechanism
In fixed guided missile.
In the above-mentioned technical solutions, transmission mechanism includes two traction devices, and a traction device is arranged in fuel charger,
The traction rope of the traction device is connect with transmission mechanism always, and the setting of another traction device is buried in magazine in target aircraft to be used
In positioning towed to transmission mechanism.
In the above-mentioned technical solutions, air refuelling adds bullet method to include following procedure:
Step 1: carrying fuel oil and guided missile by fuel charger, and flight in the sky simultaneously keeps flying with speed with target aircraft；
Step 2: fuel charger discharges rigid conduit, and with being attached for target aircraft, fuel charger discharges flexibility in rigid conduit
Oil pipe, the jet of oil filling pipe and the oil inlet of target aircraft connect；
Step 3: fuel charger discharges strut, target aircraft open in bury magazine, strut, which rises up into, interior buries magazine, strut and rigidity
Pipeline constitutes a supporting structure side by side；
Step 4: the transmission mechanism that guided missile is carried in fuel charger enters on supporting structure under the action of power drive, mesh
Magazine release traction device is buried in mark aircraft, traction device is connect with transmission mechanism；
Step 5: entering in target aircraft under the traction positioning of transmission mechanism traction device in target aircraft and bury magazine, complete
After shooting after, the traction device and transmission mechanism of target aircraft are detached from, and transmission mechanism is led under effect in fuel charger traction device
Return to fuel charger；
Step 6: after oiling, flexible tubing, rigid conduit, strut are successively recycled, completes whole process.
In the above-mentioned technical solutions, the transmission mechanism is connected as one with bracket, and transmission mechanism can be mutually with respect to bracket
Sliding.
In the above-mentioned technical solutions, the slip ring for connection, the rigid conduit on bracket are provided on the transmission mechanism
A slip ring is respectively passed through with strut, by slip ring transmission mechanism is made a relative move under external force with bracket.
In the above-mentioned technical solutions, at work, the traction device of fuel charger is in the traction device of the target aircraft
The free state of loosening draws transmission mechanism by the traction device of fuel charger when recycling.
In conclusion by adopting the above-described technical solution, the beneficial effects of the present invention are:
Different from conventional aerial oiling mode, the present invention has adds resilience energy power in the air, can be to bury magazine bullet in operational aircraft supplement
Medicine specification and quantity etc. can provide long distance to bury magazine ammunition specification and quantity etc. in operational aircraft replacement for operational aircraft
Fight one battle after another ability；
By improving to continuously perform in the single sortie of operational aircraft and appoint to bury magazine ammunition specification and quantity in operational aircraft supplement
Business ability, by reaching operational aircraft to bury magazine ammunition specification and quantity in operational aircraft replacement and not having to make a return voyage that work can be changed
War task, by for operational aircraft be operational aircraft repeatedly refueled and add bullet obtain operational aircraft single flight execute long distance
Fairly large fighting effect.
Detailed description of the invention
Examples of the present invention will be described by way of reference to the accompanying drawings, in which:
Fig. 1 is the structural schematic diagram before present invention docking；
Fig. 2 is the structural schematic diagram after present invention docking；
Wherein: 1 is the missile-borne machine that refuels, and 2 be that magazine is buried in operational aircraft, and 3 be to refuel to add missile-borne machine support, and 4 be fuelling coupling,
5 be guided missile.
Specific embodiment
All features disclosed in this specification or disclosed all methods or in the process the step of, in addition to mutually exclusive
Feature and/or step other than, can combine in any way.
Embodiment one
As shown in Figure 1, being that oiling adds missile-borne machine not complete the case where docking with target aircraft.Free flight is in fuel charger
State when, oil filling pipe and bracket are accommodated in tanker aircraft body in contraction state.When close to target aircraft need with
When aircraft docks, rigid conduit is stretched out by the control fuel charger first of control system, rigid conduit is connected with target aircraft
It connects, in order to avoid the flexible pipeline road bring tractive force of traditional approach；One end of rigid conduit is connection in the present embodiment
Onto the oil inlet of target aircraft, then connected by the oil inlet of setting pipeline road flexible and target aircraft in rigid conduit
It connects.After rigid conduit stable connection, a strut is discharged by fuel charger, strut is all rigid member as rigid conduit, branch
Bar and rigid conduit constitute a bracket, which is mainly used for the support of guided missile, complete the transfer to guided missile.
In the present embodiment, strut and rigid conduit are stretching structure；Oil transportation transmission is carried out using rigid conduit, it can be with
Solving bring when tradition carries out oil transportation using flexible duct completely has the tractive force of aircraft because using the structure of rigidity
Weight can be supported conducive to using rigid structure, to complete the replacement and increase of guided missile.
It realizes and guided missile is transferred on target aircraft from fuel charger, it is necessary first to the carrier of a carrying guided missile, only
It is only that strut and rigid conduit certainly cannot be realized, it is therefore desirable to which guided missile is arranged in transmission mechanism a transmission mechanism
It is upper to be moved on bracket by transmission mechanism, to complete the replacement of guided missile.
Because high aerial not so transmission mechanism cannot be influenced lead using the structure separated with bracket by air-flow
Cause the safety of transmission mechanism.Therefore the structure being integrally connected outside the transmission mechanism and bracket used in the present embodiment, for reality
Existing this purpose and guarantee that transmission mechanism can move on bracket, be provided with slip ring structure on transmission mechanism, rigid conduit and
Strut is each passed through a slip ring structure, and slip ring structure and transmission mechanism are the structures being fixed as one；Such connection is closed
System can ensure that rigid conduit and strut in transmission mechanism and bracket are integrated connection structure, and the work by external force
With transmission mechanism can be along bracket slide.
Realize the movement and recycling for transmission mechanism, it is therefore desirable to two sets of traction devices are set, one be set on plus
In oil machine, one is set in target aircraft.The traction end of traction device in fuel charger is kept fixed with transmission mechanism always
Connection, and connected and separated by flight control system controller between the traction end and transmission mechanism of the traction device in target aircraft.
When transmission mechanism needs mobile as target aircraft, is worked by the traction device on target aircraft, pull transmission mechanism from oiling
Machine is mobile towards target aircraft；After guided missile replacement, then pulls transmission mechanism to return to by the traction device on fuel charger and add
In oil machine.Traction device in the present embodiment can be using hoist engine and traction rope in conjunction with realizing.
Whole process are as follows:
The fixation bracket of fuel charger is connected to by flexible and positioning with the fuel tank of target aircraft first, and passes through oil transportation by fuel charger
Pipeline carries out air refuelling to target aircraft；
Traction rope is discharged by the traction device in target aircraft simultaneously, there is positioning mechanism in the end of traction rope, can accurately with biography
Transfer mechanism realizes connection, after transmission mechanism completes the load of guided missile in fuel charger, is driven by traction rope and is entered along bracket
Target aircraft, and complete the filling of guided missile；
Then it is returned in fuel charger by the traction device traction transmission mechanism in fuel charger, carries out the load of guided missile, week again
And it renews, the load until completing all guided missiles.
In this process, the guided missile loaded in target aircraft can be replaced, when transmission mechanism will be led
Bullet is sent in target aircraft, and target aircraft completes the supplement of guided missile, while the guided missile after being just replaced is loaded into transmission mechanism
On, transmission mechanism is drawn in fuel charger by traction rope, and unload the guided missile being replaced, is finally completed guided missile in cycles
Replacement.
In the whole process, in target aircraft traction device for how with transmission mechanism be accurately positioned connection ask
Topic, traction device here can use the form of mechanical-stretching bar, can also cooperate drawing head using traction rope, utilize strong magnetic
The accurate connection of location technology realization drawing head and transmission mechanism.
The invention is not limited to specific embodiments above-mentioned.The present invention, which expands to, any in the present specification to be disclosed
New feature or any new combination, and disclose any new method or process the step of or any new combination.
Claims (10)
1. it is a kind of for internally bury magazine Aircraft Air refuel plus bullet method, it is characterised in that by fuel charger in the sky with target
When aircraft is met, the connection of oil circuit is carried out between fuel charger and target aircraft using the pipeline of rigidity, is used for outside rigid conduit
The transmission of guided missile, rigid conduit are stretching structure, are stretched out by fuel charger and are connected to target aircraft, complete while carrying out oil transportation
At the transmission of guided missile.
2. a kind of method for internally burying the oiling of magazine Aircraft Air plus bullet according to claim 1, it is characterised in that
The rigid pipeline include one it is that pipeline external is set with pipeline is equidirectional carries out flexible strut, strut and pipeline structure
At the bracket for being used for transmission guided missile.
3. a kind of method for internally burying the oiling of magazine Aircraft Air plus bullet according to claim 2, it is characterised in that
The rigid pipeline includes the flexible tubing being arranged in pipeline.
4. a kind of method for internally burying the oiling of magazine Aircraft Air plus bullet according to claim 3, it is characterised in that
Described rigid pipeline one end has for the port fixed with the positioning of target aircraft oil inlet.
5. a kind of method for internally burying the oiling of magazine Aircraft Air plus bullet according to claim 2, it is characterised in that
It is provided with transmission mechanism on the bracket, retaining mechanism is provided on transmission mechanism for fixing guided missile.
6. a kind of method for internally burying the oiling of magazine Aircraft Air plus bullet according to claim 5, it is characterised in that
Transmission mechanism includes two traction devices, and traction device is arranged in fuel charger, the traction rope of the traction device always with
Transmission mechanism connection, the setting of another traction device are buried in magazine in target aircraft for positioning towed to transmission mechanism.
7. -6 any a kind of method for internally burying the oiling of magazine Aircraft Air plus bullet according to claim 1, special
Sign is that air refuelling adds bullet method to include following procedure:
Step 1: carrying fuel oil and guided missile by fuel charger, and flight in the sky simultaneously keeps flying with speed with target aircraft；
Step 2: fuel charger discharges rigid conduit, and with being attached for target aircraft, fuel charger discharges flexibility in rigid conduit
Oil pipe, the jet of oil filling pipe and the oil inlet of target aircraft connect；
Step 3: fuel charger discharges strut, target aircraft open in bury magazine, strut, which rises up into, interior buries magazine, strut and rigidity
Pipeline constitutes a supporting structure side by side；
Step 4: the transmission mechanism that guided missile is carried in fuel charger enters on supporting structure under the action of power drive, mesh
Magazine release traction device is buried in mark aircraft, traction device is connect with transmission mechanism；
Step 5: entering in target aircraft under the traction positioning of transmission mechanism traction device in target aircraft and bury magazine, complete
After shooting after, the traction device and transmission mechanism of target aircraft are detached from, and transmission mechanism is led under effect in fuel charger traction device
Return to fuel charger；
Step 6: after oiling, flexible tubing, rigid conduit, strut are successively recycled, completes whole process.
8. a kind of method for internally burying the oiling of magazine Aircraft Air plus bullet according to claim 7, it is characterised in that
The transmission mechanism is connected as one with bracket, and transmission mechanism can be slided mutually with respect to bracket.
9. a kind of method for internally burying the oiling of magazine Aircraft Air plus bullet according to claim 8, it is characterised in that
The slip ring for connection is provided on the transmission mechanism, the rigid conduit and strut on bracket respectively pass through a slip ring, lead to
Crossing slip ring makes a relative move transmission mechanism under external force with bracket.
10. a kind of method for internally burying the oiling of magazine Aircraft Air plus bullet according to claim 7, it is characterised in that
At work, the traction device of fuel charger is in the free state loosened to the traction device of the target aircraft, recycles Shi Youjia
The traction device of oil machine draws transmission mechanism.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201910398380.1A CN110239726A (en) | 2019-05-14 | 2019-05-14 | A method of for internally burying the oiling of magazine Aircraft Air plus bullet |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201910398380.1A CN110239726A (en) | 2019-05-14 | 2019-05-14 | A method of for internally burying the oiling of magazine Aircraft Air plus bullet |
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| Publication Number | Publication Date |
|---|---|
| CN110239726A true CN110239726A (en) | 2019-09-17 |
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| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201910398380.1A Pending CN110239726A (en) | 2019-05-14 | 2019-05-14 | A method of for internally burying the oiling of magazine Aircraft Air plus bullet |
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Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN115541168A (en) * | 2022-11-28 | 2022-12-30 | 中国空气动力研究与发展中心低速空气动力研究所 | Device and method for simulating free flight of wind tunnel in air refueling docking of double machines |
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| US3167278A (en) * | 1962-10-04 | 1965-01-26 | Francis D Roberge | Ordnance aerial transfer system |
| US20050145752A1 (en) * | 2003-10-15 | 2005-07-07 | Beyerle John A. | Apparatus and method for aerial rearmament of aircraft |
| US20060202088A1 (en) * | 2003-08-14 | 2006-09-14 | Nir Padan | Apparatus and method for air-to-air arming of aerial vehicles |
| US20100025523A1 (en) * | 2007-07-31 | 2010-02-04 | Kutzmann Aaron J | Reconfigurable aircraft and associated methods |
| CN103434646A (en) * | 2013-05-24 | 2013-12-11 | 北京航空航天大学 | Ammunition supply device, system and method |
| CN106143928A (en) * | 2015-04-09 | 2016-11-23 | 金嵩 | A kind of air refuelling adds bullet and air attack attack plane |
| CN106915453A (en) * | 2017-03-10 | 2017-07-04 | 佛山市神风航空科技有限公司 | A kind of takeoff and landing mode and system |
| US20180079482A1 (en) * | 2016-09-20 | 2018-03-22 | Bell Helicopter Textron Inc. | Modular Payload Systems for Aircraft |
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2019
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Patent Citations (8)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US3167278A (en) * | 1962-10-04 | 1965-01-26 | Francis D Roberge | Ordnance aerial transfer system |
| US20060202088A1 (en) * | 2003-08-14 | 2006-09-14 | Nir Padan | Apparatus and method for air-to-air arming of aerial vehicles |
| US20050145752A1 (en) * | 2003-10-15 | 2005-07-07 | Beyerle John A. | Apparatus and method for aerial rearmament of aircraft |
| US20100025523A1 (en) * | 2007-07-31 | 2010-02-04 | Kutzmann Aaron J | Reconfigurable aircraft and associated methods |
| CN103434646A (en) * | 2013-05-24 | 2013-12-11 | 北京航空航天大学 | Ammunition supply device, system and method |
| CN106143928A (en) * | 2015-04-09 | 2016-11-23 | 金嵩 | A kind of air refuelling adds bullet and air attack attack plane |
| US20180079482A1 (en) * | 2016-09-20 | 2018-03-22 | Bell Helicopter Textron Inc. | Modular Payload Systems for Aircraft |
| CN106915453A (en) * | 2017-03-10 | 2017-07-04 | 佛山市神风航空科技有限公司 | A kind of takeoff and landing mode and system |
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN115541168A (en) * | 2022-11-28 | 2022-12-30 | 中国空气动力研究与发展中心低速空气动力研究所 | Device and method for simulating free flight of wind tunnel in air refueling docking of double machines |
| CN115541168B (en) * | 2022-11-28 | 2023-03-21 | 中国空气动力研究与发展中心低速空气动力研究所 | Device and method for simulating free flight of wind tunnel in air refueling docking of double machines |
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